Airbus A320neo vs. Airbus H225 Super Puma

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Airbus A320neo versus Airbus H225 Super Puma
37.57 m 123 ft 3 in length 14.06 m 46 ft 2 in
11.76 m 38 ft 7 in height 4.38 m 14 ft 4 in
35.8 m 117 ft 5 in wingspan
2 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Turbomeca Makila 2A turboshaft engines
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 2,778 hp
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 5,556 hp
79,000 kg 174,200 lb MTOW 11,000 kg 24,251 lb
6,300 km 3,403 nm range 857 km 463 nm
M0.82 101,3 km/h cruise speed 242 km/h 150 mph
150-180 capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.